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Optimizing the trajectory of spatial movement of a flying object as a solid body

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Abstract

We consider the problem of optimal control of a flying object (FO) by the Pontryagin maximum principle with minimizing the control expenses. The dynamics of an FO in space is defined by Euler and Poisson equations. A two-point boundary value problem is solved with the Newton’s method. We give results of numerical modeling and recommendations to provide for convergence of the iterative procedure.

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Original Russian Text © S.A. Kabanov, A.A. Aleksandrov, 2010, published in Avtomatika i Telemekhanika, 2010, No. 1, pp. 46–56.

The work was supported by the Russian Foundation of Basic Research, project no. 09-08-00829.

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Kabanov, S.A., Aleksandrov, A.A. Optimizing the trajectory of spatial movement of a flying object as a solid body. Autom Remote Control 71, 39–48 (2010). https://doi.org/10.1134/S0005117910010042

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